Hydrocarbon scramjet propulsion system development, demonstration and application

9th International Space Planes and Hypersonic Systems and Technologies Conference

Volumn , Issue , 1999, Pages 1-8

  Faulkner, Robert F ^a   Weber, James W ^b  

^a PRATT AND WHITNEY   (United States)

^b AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

APPLICATION PROGRAMS; COMPUTER SOFTWARE REUSABILITY; ENGINES; HYDROCARBONS; HYPERSONIC VEHICLES; MILITARY VEHICLES; MISSILES; SPACECRAFT PROPULSION; WELL TESTING;

COMPONENT PERFORMANCE; DEFENSE ADVANCED RESEARCH PROJECTS AGENCIES; HYPERSONIC MISSILES; LIQUID HYDROCARBONS; PRELIMINARY DESIGN; SCRAMJET PROPULSION; SCRAMJET TECHNOLOGY; STRUCTURAL COMPONENT;

RAMJET ENGINES;

EID: 84983122812     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1999-4922     Document Type: Conference Paper

References (1)

1. Reddecliff, J. and Weber, J., "Development and Demonstration of a Hydrocarbon Scramjet Propulsion System," AIAA Paper 98-1613, April 1998.